Original name compressor, axial, turbine engine
A single or multistage item designed to receive, compress, and deliver air to the combustion area at a required pressure and velocity. it consists of a case (3) and vane assembly, compressor, aircraft gas turbine engine and a rotor, compressor, aircraft gas turbine engine.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 7035-01-146-7096
NSN 6145-01-594-0258
NSN 5925-01-336-1856
NSN 5835-01-246-0972
NSN 5925-01-609-3461
NSN 5935-01-111-1343
NSN 5945-01-415-6867
NSN 6220-01-608-4497
NSN 6685-01-587-6792
NSN 6105-00-007-0424
NSN 6105-01-598-1297
NSN 5855-01-550-5219